The buckling behavior of an elastoplastic cylindrical shell with a cutout u
nder pure bending was investigated analytically and experimentally. For ana
lysis, a finite element code based on an updated Lagrangian formulation was
established to analyze the problem of bending buckling by considering nonl
inear geometric and material properties. An iterative displacement-controll
ed scheme was adopted in the solution procedure to ensure the pure bending
state and to avoid numerical instability near the limiting buckling moment.
A testing device was used to perform experiments on bending buckling. The
ratio of diameter to thickness of the aluminum specimens was 50; the ratio
of length to diameter was 7.9. The shape of the cutout on the shell was cir
cular or rectangular. The influence of the size and location of the cutout
on the limiting buckling moment is discussed. Antisymmetric deformation aro
und the cutout in the shells was observed after bending buckling of the she
ll. (C) 1999 Elsevier Science Ltd. All rights reserved.